ANSIIABMA
Std. 7 - 1995
(Revision and redesignation of
ANSUAFBMA
Std. 7 - 1988)
AMERICAN NATIONAL STANDARD
ABMA STANDARD
SHAFT AND HOUSING FITS FOR
METRIC RADIAL BALL AND ROLLER BEARINGS
(EXCEPT TAPERED ROLLER BEARINGS)
CONFORMING TO BASIC BOUNDARY PLAN
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Sponsored by
American Bearing Manufacturers
Association, Inc.
Approved October 27, 1995
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NATIONAL
STANDARD
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Q Copyright 1995 hy American Bearing Manufacturers
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All rights reserved. No part of this publication may be reproduced in any form, in an electronic
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FOREWORD
This foreword is not a part of ANSI/ABMA Standard 7 - 1995, Shaft and Housing Fits for
Metric Ball and Roller Bearings (Except Tapered Roller Bearings) Conforming to Basic
Boundary Plan.
This American National Standard provides the general selection of shaft and housing fits for
metric radial ball and roller bearings of tolerance classes ABEC-1 and RBEC-1. Bearing type,
loading and other design requirements influence the criteria for shaft and housing fits.
The dimensions, tolerances and clearances stated in this standard are based on metric units and
are found in Part I of the various tables. A soft conversion to tJ.S. customary (inch-pound)
units is provided in Part II of the various tables for the convenience of the user.
Suggestions for the improvement of this standard gained through experience with its use will be
welcomed. These should be sent to the American National Standards Institute, Inc., 11 West
42nd Street, New York, NY 10036.
The officers of Accredited Standards Committee B3 operating under the American National
Standards Institute procedures and the organizations represented at the time this standard was
submitted are as follows:
W.G. Looft, Chairman
G.T. Satterfield, Secretary
American Bearing Manufacturers Association
Hydraulic Institute
Association for Manufacturing Technology
Society of Tribologists and Lubrication Engineers
U.S. Department of Defense, DISC
U . S . Department of the Navy
This~pnoductionm&bycustQnnstandruds
Services, SO2 Oakhnd Ave, Suite 5, Ann Arbor, MI 48104 (800) 699-9277, under myeky ,,qew& Nofutherreproduabnis~
ABMA (formerly AFBMA) Standards
for
Ball and Roller Bearings
1 - Terminology for Anti-Friction Ball and Roller Bearings and Parts
4 - Tolerance Definitions and Gauging Practices for Ball and Roller Bearings
7 - Shaft and Housing Fits for Metric Radial Ball and Roller Bearings (Except Tapered Roller Bearings)
Conforming to Basic Boundary Plan
8.1 - Mounting Accessories, Metric Design
8.2 - Mounting Accessories, Inch Design
9 - Load Ratings and Fatigue Life for Ball Bearings
10 - Metal Balls
11 - Load Ratings and Fatigue Life for Roller Bearings
12.1 - Instrument Ball Bearings, Metric Design
12.2 - Instrument Ball Bearings, Inch Design
13 - Rolling Bearing Vibration and Noise (Methods of Measuring)
14 - Housings for Bearings with Spherical Outside Surfaces
15 - Ball Bearings with Spherical Outside Surfaces and Extended Inner Ring Width (Includes Eccentric
Locking Collars)
16.1 - Airframe Ball, Roller, and Needle Roller Bearings, Metric Design
16.2 - Airframe Ball, Roller, and Needle Roller Bearings, Inch Design
17 - Needle Rollers, Metric Design
18.1 - Needle Roller Bearings, Radial, Metric Design
18.2 - Needle Roller Bearings, Radial, Inch Design
19.1 - Tapered Roller Bearings, Radial, Metric Design
19.2 - Tapered Roller Bearings, Radial, Inch Design
20 - Radial Bearings of Ball, Cylinder Roller and Spherical Roller Types, Metric Design
21.1 - Thrust Needle Roller and Cage Assemblies and Thrust Washers, Metric Design
21.2 - Thrust Needle Roller and Cage Assemblies and Thrust Washers, Inch Design
22.1 - Spherical Plain Radial Bearings, Joint Type - Metric Design
22.2 - Spherical Plain Radial Bearings, Joint Type - Inch Design
23.2 - Thrust Bearings of Tapered Roller Type - Inch Design
24.1 - Thrust Bearings of Ball, Cylindrical Roller and Spherical Roller Types - Metric Design
24.2 - Thrust Bearings of Ball and Cylindrical Roller Types - Inch Design
25.2 - Rolling Bearings, Linear Motion, Recirculating Ball, Sleeve Type - Inch Series
26.2 - Thin Section Ball Bearings - Inch Design
An ABMA Standard is intended as a guide to aid the manufacturer, the consumer, and the general public. The
existence of an ABMA Standard does not in any respect preclude anyone, whether he has approved the standard or
not, from manufacturing, marketing, purchasing, or using products, processes, or procedures not conforming to the
standard. ABMA Standards are subject to revision or withdrawal at any time and users who refer to an ABMA
Standard should satisfy themselves that they have the latest information from the Association.
American National Standard
ABMA Standard
Shaft and Housing Fits for Metric Radial Ball and Roller Bearings
(Except Tapered Roller Bearings)
Conforming to Basic Boundary Plan
CONTENTS
Section
Page
1. Scope ...
..l
2. Conformity with other ANSI Standards ...
1
3. Description of Shaft and Housing Tolerance Classifications ...
1
4. Selection of Shaft and Housing Fits ...
4
4.1 ShaftFi~ ...
...4
4.2 HousingFits ...
.
5. Design and Installation Considerations ...
5
5.1 Effect of Fit on Bearing Internal Clearance ...
5
5.2 Allowance for Axial Displacement ...
5
5.3 Installation Techniques ...
5
6. Symbols and Nomenclature ...
6
LIST OF FIGURES
Figure
No.
Page
1. Graphical Representation of Shaft Fits ...
2
2. Graphical Representation of Housing Fits ...
3
3. Classification of Loads in Relation to Basic Radial Load Rating C, ...
5
LIST OF TABLES
TABLE
No.
1. .Selection of Shaft Tolerance Classifications ...
7
2. Shaft Diameter Limits and Resultant Fits ...
9
3. Selection of Housing Tolerance Classifications ...
11
SHAFT AND HOUSING FITS FOR METRIC
RADIAL BALL AND ROLLER BEARINGS
(EXCEPT TAPERED ROLLER BEARINGS)
CONFORMING TO BASIC BOUNDARY PLAN
1. Scope
This standard covers the general selection of
shaft and housing fits for metric radial ball and
roller bearings of tolerance classes ABEC 1 -
RBEC 1 as influenced by the type and extent of
bearing loading and other design requirements.
Other tolerance classes are not covered by this
standard.
Recommendations for the fitting practices of
some particular types of ball and roller bearings
are covered in other ANSI/ABMA standards.
These include:
ANSUABMA
Std. No.
12.1 & 12.2
Instrument Ball Bearings
16.1 & 16.2
Airframe Ball, Roller and
Needle Roller Bearings
18.1 & 18.2
Needle Roller Bearings
19.1 & 19.2
Tapered Roller Bearings
26.2
Thin Section Ball
Bearings
This standard can also be used as a guide for
determining shaft and housing dimensions for
inch design ball and roller bearings by using
the recommended shaft and housing fits for
metric bearings and applying the appropriate
bore and O.D. tolerances for the inch design
bearings, except those bearings covered by
ANSUABMA Standard 15.
2. Conformity
with Other ANSI
Standards
In the size range O-2500 mm, the deviations
used in this standard for shaft and housing seats
conform to American National Standard ANSI
B4.2, “Preferred Metric Limits and Fits”.
3. Description of Shaft and Housing
Tolerance Classifications
In the size range described in 2 above, the
tolerance classifications are designated by a
letter and a numeral. A lower case letter is
used’for shafts and a capital letter is used for
housings. Numerals indicate the degree of
accuracy - the smaller numerals representing
closer tolerances than the larger. The letters
indicate the location of the shaft and housing
limits relative to the inner ring bore and outer
ring outside diameter tolerance ranges indicated
in Figures 1 and 2 by the symbols KB and hB
respectively.
Figures 1 and 2 show graphically how the
various tolerance classifications result in
clearance or interference depending upon how
the diameters of the mating parts interact in
specific cases.
A
INTERFERENCE
OUTER
RING
0.0.
TOLERANCE
RANGE
HoustNG
BORE
TOLERANCE
RANGES
4. Selection of Shaft and Housing Fits
To select the proper fits, it is necessary to
consider the type and extent of the load,
bearing type, and certain other design and
performance requirements.
The required shaft and housing fits are
indicated in Tables 1 and 3. The terms
“Light”, “Normal” and “Heavy” loads refer to
radial loads that are generally related to C, as
shown in Figure 3 (C,, being the Basic
Dynamic Radial Load Rating computed in
accordance with ANSI/ABMA Standards).
4.1 Shaft Fits. Table 1 indicates the initial
approach to shaft fit selection. Note that for
most normal applications where the shaft
rotates and the radial load direction is constant,
an interference fit should be used. Also, the
heavier the load, the greater is the required
interference. For stationary shaft conditions
and constant radial load direction, the inner
ring may be moderately loose on the shaft.
Table 2 shows the shaft diameter deviations and
resultant fits for the various tolerance
classifications for bore sizes over 3 mm and up
to 1250 mm.
4.2 Housing Fits. Table 3 indicates the
initial approach to housing fit selection. Note
that the use of clearance or interference fits is
mainly dependent upon which bearing ring
rotates in relation to the radial load. For
indeterminate or varying load directions, avoid
clearance fits. Clearance fits are preferred in
axially split housings to avoid distorting bearing
outer rings. The extent of the radial load also
influences the choice of fit.
Table 4 shows the housing bore deviations and
resultant fits for the various tolerance
classifications for outer diameter sizes over 10
mm and up to 2500 mm.
5. Design and Installation
Considerations
5.1 Effect of Fit on Bearing Internal
Clearance. Since interference fitting will
reduce bearing radial internal clearance, it is
recommended that prospective users consult
bearing manufacturers to make certain that the
required bearings are correctly specified to
satisfy all mounting, environmental and other
operating conditions and requirements. This is
particularly necessary in those cases where heat
sources in associated parts may further
diminish bearing clearances in operation.
Standard values of radial internal clearances of
radial bearings are listed in ANSUABMA
Standard 20.
5.2 Allowance for Axial Displacement.
Consideration should be given to axial
displacement of bearing components due to
thermal expansion or contraction of associated
parts. Displacement may be accommodated
either by the internal construction of the
bearing or by allowing one of the bearing rings
to be axially displaceable. For unusual
applications consult bearing manufacturers.
5.3 Installation Techniques. Damage to
internal bearing surfaces may result from the
transmission of mounting forces through the
rolling elements. Therefore, methods and tools
should be used that apply these forces directly
to the ring or rings being interference fitted.
To facilitate the installation of bearings on their
seatings with interference fits, bearings or
housings, as the case requires, may be
thermally expanded by heating under controlled
conditions. Bearing temperatures should not be
allowed to exceed 120°C (250°F) to avoid
‘reducing bearing hardness.
Heating of pre-lubricated bearings should be
avoided to prevent deterioration of the
lubricant. Alternatively, shafts or bearings
may be chilled to provide sufficient contraction
to facilitate installation. The bearing
manufacturer should be contacted for
information on low temperature limit and
methods of cooling. Precautions should be
observed to avoid corrosion through the
creation of excessive atmospheric moisture
condensation on bearings or other parts during
this process.
6. Symbols and Nomenclature
The following symbols and nomenclature are
used in this standard.
d
= basic bore diameter
D = basic outside diameter
C, = basic dynamic radial load rating
for a radial or angular contact ball
bearing or for a radial roller
bearing*
P = equivalent radial load*
* See ANSUABMA Standards 9 and 11 for
additional information about how these values
are determined.
BALL
BEARINGS
CYLINDRICAL
ROLLER
BEARINGS
SPHERICAL
ROLLER
BEARINGS
P/C,
Figure 3 - Classification of Load (P) in Relation to Basic Load Rating (C,)
lTABLE 1
SELECTION
OF SHAFT TOLERANCE
CLASSIFICATIONS
FOR METRIC RADIAL BALL AND ROLLER BEARINGS
OF TOLERANCE
CLASSES ABEC-1, RBEC-1
Ilt I
DESIGN &OPERATING
BALL BEARINGS
CONDITIONS
1
Rotational
Conditions
Inner Ring
Axial
Diiplaceabillty
Radial
1
d
1 Tolerance
Loading -
Over
Inner Ring
Rotating
in relation
to Load
Direction
Light
’
18
OrNormal
1:
Load
Direction
is
Indeter-
minate
Heavy
1:
Inner Ring
StationaT
in Relation
to Load
Direction
Inner Ring must
be easily axially
displaceable
Inner Ring need
not be easily
axially
displaceable
Pure Thrust (Axial) Load
Light
-
Classification
Incl.
(1)
18
h5
All
j6
(2)
18
j5
All
k5
Loo
k5
All
m5
zerrn:’
/
All Sizes
1
g6
CYLINDRICAL
ROLLER BEARINGS
T
d
Over
Incl.
0
40
40
140
140
320
320
500
500
All
0
40
40
100
100
140
140
320
320
500
500
All
0
40
40
65
65
140
140
200
200
500
500
All
All Sizes
All Sizes
Tolerance
Classification
(1)
$X2)
W2)
W2)
z
k5
m5
m6
n6
~6
r6
m5
m6
n6
p6
r6
r7
h6
Consult Bearing Manufacturer
SPHERICAL
ROLLER BEARINGS
d
Tolerance
Classification
Over
Incl.
(1)
0
40
$32)
40
100
W2)
100
320
mW)
320
500
n6
500
All
~6
0
40
k5
40
65
m5
65
100
m6
100
140
n6
140
280
~6
280
500
r6
500
All
r7
0
40
m5
40
65
m6
65
100
n6
100
140
~6
140
200
r6
200
All
r7
All Sizes
86
All Sizes
h6
Dimensions in millimetres
(1) Tolerance Classifications shown are for solid steel shaft.. Numerical values are listed in Table 2.
For hollow or nonferrous shafts, tighter fits may be needed.
Pa
Irt IT.__
--
TABLE 1
SELECTION
OF SHAFT TOLERANCE
CLASSIFICATIONS
FOR METRIC RADIAL BALL AND ROLLER BEARINGS
OF TOLERANCE
CLASSES ABEC-1, RBEC-1
Dimensions in inches
DESIGN &OPERATING
BALL BEARINGS
CYLINDRICAL
SPHERICAL
CONDITIONS
ROLLER BEARINGS
ROLLER BEARINGS
Rotational
Inner Ring
Radial
d
Tolerance
d
Tolerance
d
Tolerance
Conditions
Axial
Loading
Classification
Classification
Classification
Displaceabillty
Over
Incl.
(1)
Over
Incl.
(1)
Over
Incl.
(1)
0
1.57
j6(2)
0
1.57
$32)
Light
’
0.71
h5
1.57
5.51
WV
1.57
3.94
W2)
Inner Rinrr-
0.71
All
j6
(2)
5.51
12.6
mG9
3.94
12.6
m6(2)
Rotating
12.6
19.7
n6
12.6
19.7
n6
in relation
19.7
All
~6
19.7
All
~6
to Load
Direction
0
1.57
3.94
1.57
k5
m5
0
1.57
2.56
1.57
k5
m5
Normal
0
0.71
j5
3.94
5.51
m6
2.56
3.94
m6
0.71
All
k5
5.51
12.6
n6
3.94
5.51
n6
or
12.6
19.7
~6
5.51
11.0
~6
19.7
All
r6
11.0
19.7
r6
&&
19.7
All
r7
Direction
0
1.57
m5
0
1.57
m5
is
1.57
2.56
m6
1.57
2.56
m6
Indeter-
0.71
3.94
k5
2.56
5.51
n6
2.56
3.94
n6
minate
Heavy
3.94
All
m5
5.51
7.87
~6
3.94
5.51
~6
7.87
19.7
r6
5.51
7.87
r6
19.7
All
r7
7.87
All
r7
Light
Inner Ring must
be easily axially
Normal
All Sizes
86
All Sizes
All Sizes
g6
Inner Ring
displaceable
Stationary
Heavy
in Relation
to Load
Direction
Inner Ring need
Light
not be easily
axially
Normal
All Sizes
h6
All Sizes
h6
All Sizes
h6
displaceable
Heavy
Pure Thrust (Axial) Load
All Sizes
j6
Consult Bearing Manufacturer
(1) Tolerance Classifications shown are for solid steel shaft.. Numerical values are listed in Table 2.
For hollow or nonferrous shafts, tighter fits may be needed.
TABLE 2
SHAFI’ FIlTING
PRACTICE
FOR METRIC RADIAL BALL AND ROLLER BEARINGS
OF TOLERANCE
CLASSES ABEC-1, RBEC-1
Part I
r
I
TOLERANCE CLASSIFICATIONSd
16
h6 h5 .js16
ks k6 mS m6 n6 p6 r6 I7Devi- Shaft Rwul- Shaft Raul- ShnR Red- Shaft Red- Shaft Rest& Shaft Red- Shnfi Raul- ation Lkvi- tan, Devi- *ant Dwi-
Shah Red- Shaft Red- Shaft Red- Shaft Raul- ShnR Resul- Shaft Raul- ,.“, Derl- *a”, Devi- tan, DWI- tsnt Devi- tant DA- tant Devi- tsnt Lkvi- tan, Dtri-
stion Fit stion Fit stion Fll nilon Fit stion Fit ation FR tant tkvi- tan, Devi- tant 131
ation M hm --- Fit SO”” m ---. - --
stinn M --.-..
ation Fit ation Fit ation Fit 1 0 -4 I2L 0 0 +3 +6
1
I61
1 1 -12 1 , 4T 1 1 -8 1 1 8LI WI -5 t 1 5L1 ST 1 I 2Li -21 IITI 1 2L1 t6 I ITI -21
I4T1 +I I I4Tl I1
I 1 +9 1 I -- 47 I 1 I I I I I I -81
Iiillnl
I
I
I
I -.. ._ . . . I 6 0 -5 14L .i 9L -: 6L t4 2L +7 2L +7 1:: +12 6T IO -8 -14 3T 8T 8T -2 12T -2 IST +I t6 2OT IO 0 -6 17L 0 IIL 0 8L +5 3L t8 3L +9 IT +I5 I8 -8 -17 2T -II ST -8 8T -3 l3T -3 l6T +I 17-r t7 2:: I8 0 -7 2OL 0 l3L t5 4L t9 4L fll 2T I +17 I RI- 80 -15 -29 ST -19 15T -1 2lT -7 27-T t2 80 0 -12 34L 0 22L +6 9L t13 +I8 120 -20 -34 8T -22 2OT -9 26T -9 3:; +3 I20 0 -14 39L 0 25L t7 IIL t14 IIL t21 I80 -25 -39 IIT -25 25T -II 32T -II 39T +3 180 0 -I5 44L 0 29L +7 l3L +I6 l3L t24. 30 -10 -20 3T -13 1 IOT -4 IST -4 l9T t2 21T +8 2% 30 0 -9 25L 0 16L +6 5L tll 5L +13 2T +I8 2T +20 +25
50 -14 -25 3T -16 l2T -5 I8T -5 23T t2 25T t2 30T t9 3: t9 3:
50 0 -10 29L
01
l9L t6 7L t12 7L +I5 2T t21 2T +74 IIT t30 IIT +39 20T I 39T +I1 45T t20 54T D I-- ?L I . . . t45 23T t59 37-r --- -- ~~~ -1. .” .-. ,_ -l. . . ~~, , t23 651-1 +37, 79-r,I
I
I
3T t28 3T +33 IST t40 l5T +52 27T, t68 1 43T 1 +!Xl , 65T, 46T t3 53T +15 58T +I5 65T t27 77T 1 +43 i 93T 1 t65 1 I I5T II
I
r
I4T +37 I7T t46 ITT 1 +M) 1 31T 1 +79 1 SOT, tlC.5 1 77T I
I
I
54T +17 f.,+ 117 x7’ *>’ ’ 9iJT 1 t50 1 lO9T 1 t77 I 1361 I
I
I
1
1 2W 1 -30 1 ~44 1 15T I -29 , 30T 1 , 1 -I3 1 VT, -I3 1 46T1 -. +4 1 _.. I.
I.1
.
.-.
,~.
200
1
1 0 1 -15 1 44L 1 0 1 29L 1I
1 +71 l3Ll +I61 l3LI t241 4T11
I t37l1x1 +4flI
1x1 -CAnI-. .~. .- -. _._ I . . . 1.. I.. ,“, ,-,
225 1 1 0 1 -15 1 44L
1
0 1 29L I I 1 t7 1 l3L, +I6 1 l3L I t24 1 4T iI
1
+37l l7Tl +4nl 17rl +mI1
1 225 i -30 1 -44 1 IST 1 -29 1 3OT 1 I 1 -13 I 37T I -13 I 46T I +4 i 54T.I I1
1 250 1 -30 1 -44 1 IST 1 -29 1 3OT i 11
-13I
37Tl -I3I
46Tl +4 1 5ATl I 1 280 1 -35 1 -49 1 l8T 1 -32 1 35T 1 I 1 -16 1 42T 1 -I6 1 5IT 1 +4 11
280 1 1 0 1 -17 1 49L 1 0 1 32L i 1 +7 -. ..~ .- .-. _.. I . . . “.. ..I ,“. ,~, 250 1 1 0 1 -17 1 49L 1 0 1 32L 1I
1 t7 I l6L 1 +I6 I l6L 1 t27 f 4T I1
1 +43 I 20T 1 t57 1 7”T I +.M 1315
355
400
-ir
I6L +I6 l6L t27 35T -16 42T -16 SIT t4 36L t7 I8L +I8 l8L t29 4oT -I8 47T -18 58T t4 36L +7 I8L +I8 l8L t29 40T -I8 47T -18 58T t4 4OL +7 2OL +20 2OL t32 45T -20 52T -20 65T t54OL t7 2OL t20 2OL t32 .I. .“I
SW -45 -60 2ST -40 45T -20 52T -20 65T t5 7TT. +23 95T t40 l25T t68 l53T ““. tl32 , ,,- 217T l32T +I32 +I95 2401 I321 500 0 -22 66L 0 44L 22L t22 22L t30 t56 26T +122
SM) -50 -6.5 28T -44 SOT 58T -22 72T 0 +26 IO6T t7.5 l72T 7ar +194 +I50 244T ISOT t220 tl50 27o1 l5Ul SKI 0 -22 66L 0 44L +8 22L t22 22L t30 i-56 26T t122 78-r t199
630 -50 -66 28T -44 SOT -22 58T -22 72T 0 8h +26 lO6T +7cl l72T +I55 249T l55T +225 +I55 275’1. IS5 I 630 0 -24 74L 0 SOL t10
1
25L 1 t251
25L 1 +35 I 0 I I I -CM I-- --.
UIT, I I I710 -75 -74 SIT -50 75T -25 1 85T 1 -251 IcuTl 01 II&
I
+30 l4OTI
I
I
;g;: 710 0 -24 74L 0 5OL t10 1 25L 1 t25 I 25L I t35 I ” I85Tj Roll
--- -75 - -70 <IT -. -5” _” XT .-. I -2s 1 ~~~
-ii 1 IOOT( 0 1 IIOT
I
I +fx I %IT I
+Gi
1-_’
14OT
1
I
I
I
I S-Y YYI IL>> 102,’ +265 1851. t&8 213T +I85 3lOT +I85 340 I 801-1 1 1 0 -26 .I 821. 1 0 1 56L 1 1 +I2 28L t28 28L t40 0 +74 34T +I56 IOOT t266
900 -IW -82 74T -56 1 IWT 1 i -20 ll2T -28 l2liT 0 l4OT +34 l74T +Wl .-- lwi- --_. +,tn .-._ ,c4.T _“I. 2lOT t3GU A,,” ,c,” !lW’ “,YYl -L”,,
TABLE 2
SHAFT FITTING
PRACTICE
FOR METRIC RADIAL BALL AND ROLLER BEARINGS
OF TOLERANCE
CLASSES ABEC-1, RBEC-1
Dimensions m lnclws Deviakmsr and Fits in O.ooOl lncl~s d
I
TOLERANCE CLASSIFlCATlONS I
g6
h6 N is j6 Its k6 ms m6 n6 p6 r6 r7Devi- Shaft Red- Shaft Red- Shaft Rest& Shaft Raul- Shaft Red- Shaft Red- Shaft Red- Shaft Red- Shaft Rsul- Shaft Red- Shaft Red- Shaft Red- Shaft Red- ario” Devi- tant Devi- tan, Devi- tnnt Devi- tani &vi- tant lkvi- tnnt Lkvi- tmt &vi- tan, Devi- tant lkvi- tant De+ tant DA- tan, Devi- tant ation Fit stion nt atian Fit atlon Fit ation Fit stion Fit ation Fn ation Fit ntion Fit stion Fit stillon Fit stian Fit ntion Fit
I i ~~~~ ~~~ ~~~~~ i 0 5L 3L 2L +I IL +2 IL +2 OT +4 2T -3 :: IT .i 3T -i 3T -I 4T -I 5T 0 ST +2 -IT -2 6L 0 4L 0 t2 IL +3 IL t3 OT ::: -I ST -I 6T 0 6T t5 2T -6 IT -4 3T -2 +2 8T -2 7L 0 4L 3L t2 IL t3 IL t4 OT .; 3T -I ST -I 6T 0 7T +6 -7 IT -4 3T +3 0 -3 8L 0 t2 2L +4 2L +4 t7 3T -4 -8 IT -5 -2 6T -2 8T +I :$ +3 IIT 0 -4 IOL 0 6L t2 +4 t5 +7 +S 4T +10 4T -4.5 -10 0.5T -6 4.5T -2 6.::: -2 8.::: +I 9.:T +I Il.:% +4 l2.5T t4 l4.5T 0 IIL 0 7L +2 3L +6 t9 4T +I2 t15 -6 .i: 2T -7 6T -3 IIT +I I:; +4 IST +4 I:: t8
0 -5 13L 9L .i ST
+2 4L t5 4L t7 IT +I0 IT +ll ST +I4 +I8 2:: +9
W t23 IST -8 -13 3T -4 IOT -4 l3T +I IST +I l8T +5 l9T t5 26T +I5 3lT
0 -6 l5L 0 IOL +3 4L +6 4L t8 IT tll 1T +I3 6T t16 IIT +27 IiT +35 267 -IO -I5 4T -10 IOT -4 l3T -4 l6T +I I8T +I 21T t6 23T +6 30T +I7 37-l’ +26 45T 0 -6 l7L 0 IIL t3 5L +6 5L t9 2T +I5 7T +I8 ?T +24 l2T +3l 20T +42 30T .I) 1 -17 i hT i -,I 1 l2T1 1 I -5 I IST I -5 I l8T1 t2 I 2lT1 I
, -3 -. .-. -~
1 -6 1 l7L i 0 I IILI I 1 +3 1 5Lt +6 1 5Li +9 1 2TI
I
1 +I5 I 7T I +I8 1 7T I t24 I l2T 1 +3l I 2UT1 t43 I 0-I2 -17 6T -II l2T -5 IST -5 I8Tj +2 21T 0 -6 l7L 0 IIL t3 5L +6 +9 2T -I? -17 6T -II l2T -5 IST -5 1::: t2 21T 0 -7 19L 0 l3L +3 6L t6 6L +II 2T -1.4 -10 lT -11 IAT -6 l7T -6 2OT +2 25T
1 +7 1 27T1 +7 1 30T 1 +I2 1 36T1 +20 1 43T1 t3l I
+I5 7-I’ +I8 7T t24 I2T t31 2l-n t44 33T +5l 33’1 +7 27-r t7 30T +I2 36T t20 43T +33 S6T +33 hTl
I
+17 8T +20 8-T 1 +26 l3T -I 1.. ,
-
.
0 II
-7I
I
l9L77
I
I
0 I
I
13LI
I
I
I
1 1 +3 1 -61 6L1 t6 1 6L1 tll.,4
-10
,
-II
. _
IdT
. .
I7Tl0 I -7
I
2lLl01
l4LI 1 1I .li I
I
I
-16
-9,QT
I.w
I
I
I
t3 -71I
IWI 7L I +7I
7Ll +I1 0-16
1 -1; 1OT I .I; I IfiT I
I
I
-8 I
l9TI -7 1 23T 1 +Z 1 77l’II
‘-
_. _. . ._. a . _. I
I -7 I 2lL
I
0 I
14LI
I
1 t3 1 7Li +7 1 7L1 +II I 2T1I
I -I
_. , . . . . “ . - _.. ._ _.. - - . - . -- -
-1;
-8 24L 0 I6L +3 8L +8 8L +I3 $20 9r t31 l6T t43 2TT +65 JUI T,., ,I,, -24 IOT -16 l&T -8 21T -8 26T +2 3:; +9 38T +I6 49T t27 6lT t50 83T +50 92-r 0 -8 24L 0 I6L +3 +8
-I8 -24 IOT -16 IST -8 2;; -8
8L +I3 +20 t31 16T t43 27T t68 52T t77 52’1 26T +2 3:; t9 3;: +I6 49T +27 6lT +52 86T +52 95’1 n -9 7hl ” 171 t3
I
9L t9 9L +12 0 I +22 IOT +AR 1 1IT +7h WT +I77 COT1 +7 1 27Tl t7 I 30T I +I2 I 36TI +20 I 43TI t30 I 54T
._ _..
I
-18 -CR -SAT ST t29 +I5 ACT IST +39 &,A : 1 1 +I7 I ST I +20 I 8T I t26 I l3T 1 -I 1 +R 1 ._ 3lTI ..~ t8 I 34T 1 +I? 1 4Crl-1 Ii +I8 1 8T 1 +22 1 ST I +29 I 15T 1 -I
I
+R 1 UT1 +R I 1RTl +I5 I ACTI +,A-2;
0 -20 0 -26 -2 -9;iT -Ii iar
-9 23T -9 29T 6 3iT .__ ._ . +10 42T +3l 68T t59 96-k +$I 1071 _‘. 26L 0 l7L t3 2:: +9 9L +12 3;T +22 lm- +48 3lT t78 61T t89 61’1 IIT -17 2oT -9 -9 29T 0 +10 42T +31 68T t6l 98T t6l 109.1 29L 0 2OL 1 +4 IOL +I0 IOL +I4 0 t26 12T t54 1 35T +89 69T +I00 69T 30T -IO 34T -10 40T 0 4AT I I I II, , I .A , I .a”. <AT I I I I I I I I r-i< Ia., I “7. P”T I ILCI I”, ll9T t69 l3OJ 2OL t4 IOL +10 IOL t14
-10 40T 0 :T I t26 l2T MT -IO 34T +I2 56T I I +s4 35T t93 73T +I04 73T +35 84T +73 I23T t73 l34T 22L -::
IIL +I1 IIL +I6 0 I
I
1 t29I+131
I 68~1 l3T II
II
II
I 1 t6l 1 +39 1 IOOT I +83 1 39T It105 83T +I18 83T39T 44T -II 5crT 0 55T 144T +83 1571.
TABLE 3
SELECTION
OF HOUSING TOLERANCE
CLASSIFICATIONS
FOR METRIC RADIAL BALL AND ROLLER BEARINGS
OF TOLERANCE
CLASSES ABEC-1, RBEC-1
DESIGN AND OPERATING
CONDITIONS
TOLERANCE
Rotational
Conditions
Loading
Other
Conditions
Outer Ring
Axial
Displaceahility
CLASSIFICATION
(1)
Light
Normal
or
Outer Ring
Heavy
Stationary
in relation
to load
direction
Shock with
temporary complete
unloading
Heat input
through
shaft
Housing
split
axially
Housing not
split
axially
Outer ring
easily axially
displaceable
G7 (3)
~57 (2)
r-I6 (2)
56 (2)
Load
Direction
indeterminate
Outer RinK
in
Rotatinr:
relation to
load direction
Light
Normal or heavy
Heavy shock
Light
Normal or heavy
Heavy
Transitional
range (4)
K6 (2)
Split
not
Mf5 (2)
recommended
N6 (2)
_
Outer ring not
Thin wall
easily axially
housing not
displaceable
~‘6 (2)
split
(1) For cast iron’ steel housings. Numerical values are listed
in Table 4. For housings of non-ferrous alloys tighter fits may
be needed.
(2) Where
wider tolerances are permissible, use tolerance classifications H8, H7, 57, K7, M7, N7 and P7 in place of H7, H6,
56, K6, M6, N6 and P6 respectively.
(3) For large bearings and temperature differences between outer ring and housings greater than 10 degrees C, F7 may be
used instead of G7.
TABLE 4
HOUSING Fi’ITING
PRACTICE
FOR METRIC RADIAL BALL AND ROLLER BEARINGS
OF TOLERANCE
CLASSES ABEC-1, RBEC-1
Dimensions III M~ll~mctrrs Part I
I 1 TOLERANCE CLASSWICATIONS
d
F7 G7 H8 Hl H6 J6 17 K6 K7 M6 M7 N6 N7 P6 17
Holaing Rerul- Housing Red- Housing Raul- Homing Red- Houring Red- Houdng Red- Housing Resul- Holaing Raul- Housing Rsul- Housing Red- Housing Raul- Houhg Red- Housing Red- Housing Raul- Housing Hrsul- over inch 211; Devi- tan, Devi- tl”t Devl- tant Devi- tant Devc tant Devi- tant nevi- tnnt lkvi- tmll nevi- tant Devi- tn”t Devi- tant Jkvi- tmt Devi- tant Devi- tnnt Devi- ,a,,,
ntion Fit ation FM at ion Fm .stion Fit ation Fit atlon Fit atlon Fit ation Fit ation Fit ation Fit stion Fn ation Ftt ation Fit ation Fit atiun Fit IO +o +I6 42L +6 32L 0 3.5L 0 26L 0 19Ll -5 1 14LI -8 1 18LI -9 1 IOLl -12 1 14L1 -15 1 4L1 -18 1 SLI -20 I IT/ -23 1 3L1 -26 I 7Tl -251
I 3rl
I8 -8 t34 16L +24 6L +27 0 +1a 0 +I1 0 t6 ST +I0 8T +2 9T t6 127 :; 157 -0 1iT -9 2OT -5 23T -15 26T -II 29 1~ 18 +o +20 SOL f7 37L 0 42L 0 3OL 0 22L -5 l7L -9 21L -I1 IIL -15 15L -17 5L -21 9L -24 2T -28 2L -31 w -35 5 I
30 -9 +41 20L +28 7L +33 0 +21 0 +13 0 +B 5T +12 9T +2 IIT t6 IST -4 17T 0 21T -11 24T -7 28T -18 3lT -I4 351 30 +o +25 611. +9 45L 0 SOL 0 36L 0 27L -6 2IL -11 25L -13 14L -18 18L -20 7L -25 1IL -28 IT -33 3L -37 imr -42 61. 50 -II t50 25L +34 9L t39 0 +25 0 +I6 0 +10 6T t14 11T +3 13T +7 IaT -4 2OT 0 25T -12 28T -8 33T -21 37T -17 42 I 50
I
I
to
I
t30I
73LI +I0I
53LI0 I
59Ll0 1
43LI0 1
32LI -6 1 26Lj -121
31LI -151
17LI -211
22L/ -24 1 8Ll -30 l 13Ll -33 l ITI -39 I 4L1 -45 I 13T1 -51 I 8rl 80 -13 +64-J 3OL +40 IOL +46 01 t30 0 t19 0 +13 6T 1 +I8 1 12T1 t4 1 l5Tl t9 1 21T -5 24T 0 3uT -14 33T -9 39T -26 4sr -?I 51’1‘ 80 +o t36 86L +12 62L 0 69L 0 5OL 0 37L -6 31L -13 37L -18 19L -25 25L -28 9L -35 ISL -38 IT -45 5L -52 l5T -59 Yl120 -15 t71 36L t47 12L t54 0 +35 0 t22 0 +I6 6T +22 13T +4 18T t10 25T -6 28T 0 35T -16 38T -10 45T -30 52T -24 59T 120 .:i 1:: %i 1:: ::t, t6: 8lL 0 58L 0 43L -7 36L -14 44L -21 22L -28 3OL -33 IOL -40 18L -45 2T -52 6L -61 l8T -68 ILrI 1 150 t ._. .- 1 -- 1 ~~ 1 ]
0 I
+401 01 +25l O] +18] 7T] t26 ] 14T] t4 ] ZIT] +12 ] 2gTl _. -8 I 33TI 01 4oTI .~ -20 I 45T1 t -12 I 52T1 -36 I 6lTI -28 I 68’1 II
I50 to t43 IOBL t14 79L 0 88L 0 65L 0 SOL -7 43L -14 5lL -21 29L -28 37L -33 17L -40 25L 45 5L -52 13L -61 I IT ~68 3.1 I80 -25 +a3 43L +54 l4L +63 0 +40 0 +25 0 +I8 7T t26 14T +4 21T +I2 28T 8 33T 0 407 -20 45T -12 52T -36 6lT -3 681 I80 I I +0 I t50 I l26Ll +I5 I 9lLI 0 , lO2Ll 0 I 76L1 0 , 59L, -7 , 52L, -16 , M)L, -24 , 35L, -33 I 43L. -37 n 22L. -46 . 30L. -51 , 8L. -60, IbL. -70 m IIT. .79. 3.1‘ I
250 -30 t96 SOL t6l ISL t72 0 t46 0 +29 0 t22 n- t30 1 16TI t5 1 24TI +13 1 33T -8 37T 0 46T -22 1 51T 1 -14 6OT -41 70T -33 7Yl 250 +o t56 l43L t17 lo4L 0 l16L 0 87L 0 67L -7 6oL -I6 7lL -27 4OL -36 SlL -41 26L -52 35L -57 IOL -66 21L -79 I2T -88 I I’
31s -35 +I08 56L +69 l7L +a1 0 t52 0 t32 0 t25 ?T +36 l6T t5 27T +I6 36T -9 4lT 0 52T -25 57r -14 66T -47 79T -36 881’ 315 to i62 l59L +I8 ll5L 0 129L 0 97L 0 76L -7 69L -18 79L -29 47L -40 57L -46 3OL -57 4OL -62 14L -73 24L -87 trr -98 II
400 -40 t119 62L t75 I8L +89 0 t57 0 t36 0 t29 7T +39 18T +7 29T t17 4oT -10 46T 0 57T -26 62T -16 73T -51 87T -41 YBI’
scml I +o I +76 1 I%Ll t22 I l42LI 0 I l6oLl 0 I IZOLI 01 94L.l -7 1 87LI -22 1 98L1 -44 1 SOLI -70 1 5OL1 -70 1 24LI -% 1 24LI -88 I 6L1 -114 I 6L1 -122 I 28T1 .I48 I 630 -50 t146 76L t92 22L +I10 0 +70 0 +4l 0 +37 7T +40 22T 0 44T 0 703 -26 7oT -26 %T -44 88T -44 ll4T -78 I227 -78 I4XI 630 +o t80 2351. i-24 l79L 0 2cQL 0 l55L 0 125L -10 I15.L -24 131L -50 75L -80 75L -80 4SL -110 45L -100 25L -130 25L -138 l3T -168 131~
8crJ -75 t160 8OL +Iw 24L t125 0 trio 0 t50 0 t40 IOT +56 24T 0 SOT 0 SOT -30 am -30 IIOT -50 IOUT -SO 13OT -88 138T -88 l68I ml +o t86 276L t26 216L 0 240L 0 ISQL 0 156L -10 146L -26 164L -56 IM)L -90 ICCJL -90 66L -124 66L -112 44L -146 44L -156 0 -IYU 0
IO00 -loo +I76 86L +I16 26L +I40 o t9O o +56 0 t46 IOT +64 26T 0 56T 0 9OT -34 9OT -34 124T -56 ll2T -56 l46T -100 156T IOU Iyol~
1 I -3
IOOII +o t98 328L t2a 258L 0 2WL 0 230L 0 191L -10 ISIL -28 2u2L -66 125L -105 125L -1% 85L -145 85L -132 59L -171 59L -186 5L -225 SI. 1250 -125 +203 98L t I33 28L +I65 0 t105 0 +66 0 t56 IOT +77 28T 0 66T 0 IMT -40 lO6T -40 145T -66 132T -66 l71T -120 I86T -110 ??ST I250 I I to I t110 I 395Ll t30 I 315LI 0 I 355Ll 0 1 285Ll 0 1 238Ll -10 1 228Ll -33 1 255Ll -78 1 IaOLl -125 1 l6OLl -126 I 112L1 -173 1 112L1 -156 1 82Ll -203 I 82L1 -218 1 2OL1 -265 I !I)1 I
l6NJ -160 t235 IIOL +I55 3OL t195 0 t125 0 t78 0 t68 IUT t95 3UT 0 7gT 0 125T 48 126T -48 173T -78 156T -78 203T -140 2l8T -140 265-l I603 to +I20 470L +32 382L 0 43OL 0 35OL 0 292L -10 2821, -32 318L -92 2ooL -150 2rmL -150 142L -208 142L -184 108L -242 108L -262 3OL -320 301 ?oM) -2oo t270 IZOL +I82 32L +230 0 +150 0 +92 0 +a2 IOT +llg 32Y 0 92T 0 ISOT -58 ISOT -58 2olrr -92 MT -92 242T -170 262T -171) 3!01- !cKw 0 t130 555L t34 459L 0 53OL 0 425L 0 360L -10 3SOL -34 391L -110 25OL -175 25OL -178 l82L -243 182L -220 14OL -285 l4OL -305 551. -3711 551 25W -250 t305 l3OL t2o9 34L +280 0 +175 0 t110 0 +I00 IOT +I41 MT 0 llcrr 0 17ST -68 l78T -68 243T -110 22aT -110 285T -195 305T -11)s 3711 I L= Lmse. T= Tight